Overview

Data on design, manufacture and status

Latest or last design authority: Airbus Helicopters
Originally designed by Société Nationale Industrielle Aérospatiale

Latest or last primary manufacturer: Airbus Helicopters
Originally manufactured by Société Nationale Industrielle Aérospatiale

Parent type: Airbus Helicopters H155/EC155/AS365/SA.365

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 4.06 m (13.3 ft)

Overall Length: 13.73 m (45.0 ft)

Overall Width: 11.94 m (39.2 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Arriel 2C turbine

Engine manufacturer: Turbomeca

Max continuous power: 581 kW (779 hp)

Take-off / rated power: 626 kW (839 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 4300 kg (9480 lb)

Max Gross Weight (airborne): 4250 kg (9370 lb)

Max Range: 792 km (428 nm)

Max Endurance: 4.1 hrs (4.1 hrs)

Related VFS Resources

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Related Public Resources

Resources related to the AS365 N3+ Dauphin, provided by public sources across the internet.

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